04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017156 AERAZUR - ZODIAC AEROSPACE EASA.R.S.01263 REV. 4 S-92A Installation of AERAZUR Internal Auxiliary Fuel The IAFS Completion Kit can be installed only Prior to installation of this modification it 10.03.2011 GROUP System (lAFS) completionkit pin 508617 or on S-92A helicoptersequipped with: - must be determined thatthe 508617-1 or 508617-2 or 508617-3.Revision 4 AERAZUR IAFS Provision Kit p/n 509429-02 interrelationship between thismodification of STC introducing new kit pin 508617-3 and or 509429-03, approved underSTC 10017259 and any other previously installed reviseddocumentations Revision 3 or later-S-92A Avionics modification and/ orrepair will introduce Management System (AMS) version n° 091- no adverseeffect upon the airworthiness 2527-007 or latera of the product.IAFS com 10017259 AERAZUR - ZODIAC AEROSPACE GROUP EASA.R.S.01466 REV. 6 S-92A Installation of Provision Kit p/n 509429-03 of Internal Auxiliary FuelSystem (IAFS).STC Revision 5 introduces minor design modifications, reviseddocumentation and revised limitations for compatibility with S-92A cabininterior panels. 10014306 AERLYPER S.A. EASA.A.S.01550 BEECH 200 Installation of MST67A Transponder Mode S Equipment. 10014317 AERLYPER S.A. EASA.A.S.01567 BEECH 200, SUPER KING AIR Tactical console installation on B-200 aircraft In accordance with Doc. No. 100528 "Aircraft with ARGOS system, tactical communications Flight Manual Supplement", Issue 01, 27 system and fixed provisions for ASTRA system. November 2006. 10014318 AERLYPER S.A. EASA.A.S.01568 BEECH 200 Inmarsat SATCOM installation on board In accordance with Doc. No. 100429 AFM B200.The modification is optional and fixed. It consists of an Inmarsat SATCOM terminal to be installed in the passenger cabin. A SATCOMantenna is installed on the upper part of the fuselage. Supplement ED.03. 10014319 AERLYPER S.A. EASA.A.S.01569 BEECH 200 Installation of New Avionics Equipment to comply with COM/NAV regulations for IFR and B-RNAV Operation. 10014420 AERLYPER S.A. EASA.A.S.01741 FAIRCHILD SWEARINGEN SA Garmin GPS 155XL with antenna GA-56, Mid- The aircraft is approved for dual pilot B-RNAV 227-BC Continent MD41-448 Annunciation control Unit operation, subject to the conditions, limitations and copilot CDI Mid-Continent MD 40-09L and procedures contained in Doc NoAI03-081installation for B-RNAV operation 03 "Flight Manual Supplement", Rev 03 10017103 AERLYPER S.A. EASA.R.S.01073 EC 135 P2 Microwave Transmission System on EC-135 Helicopters 10017104 AERLYPER S.A. EASA.R.S.01075 BO105 C, BO105 S ASTRA System installation on BO-105 C/S Helicopters 10017105 AERLYPER S.A. EASA.R.S.01076 EC 135 P2 Installation of Image Recorder System UM III and Options System 10017137 AERLYPER S.A. EASA.R.S.01231 BO 105 C, BO 105 S Digital microwave transmission system installation on board BO-105 C/S. 10017197 AERLYPER S.A. EASA.R.S.01338 REV. 1 EC-135-P2 (CPDS) EC-135-P2+ UM-III HD Camera System & Microwave Transmission System Installation Onboard EC135. 10033659 AERLYPER S.A. P-EASA.R.S.01507 REV. 1 EC135 P2 & EC135 P2+ Installation of STAR SAFIRE HD Camera System & Digital TransmissionSystem 10015649 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01624 REV 1 TCCA STC C-LSA05-303/D ISSUE 2 BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration 10015653 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01628 REV 1 TRANSPORT CANADA STC C-LSA05- BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior 2 Configuration Refer to attached table. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 23.07.2012 06.12.2007 31.05.2007 31.05.2007 06.12.2007 17.01.2006 In accordance with Doc No 100198: RFM 14.02.2006 Supplemt Ed. 3 In accordance with Doc No 100137: RFM 30.01.2006 Supplement Ed.4 Doc No 100059: RFM Supplement Ed. 3 08.02.2006 In accordance with Doc. No. 100589 "Aircraft Flight Manual Supplement", issue 1, April 2008.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed mod 1. Master Data List and RFM Supplement mentioned above. 01.07.2008 13.05.2008 None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 02.03.2011 Restricted to Aircraft Serial Number 5610 25.07.2006 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.2. Restricted t 04/01/2013 Page 8/462 25.07.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015670 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01647 REV 1 TCCA STC C-LSA05-317/D ISSUE BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior 1. Restricted to ASN 5620 only.2. This STC is 10.08.2006 Configuration approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the 10015671 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01649 REV 1 TCCA C-LSA05-315/D ISSUE 2 BOMBARDIER CL-600-2B16 (CL- 604 Aircraft Completion 12 Passenger Interior Configuration 10015678 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01659 REV 1 TCCA STC C-LSA05-328/D BOMBARDIER CL-600-2B16 Aircraft Completion 12 Passenger Interior Configuration 1. Restricted to ASN 5612 only2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the i 1. Limited to S/N 56172. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the ins 10015859 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.01967 TCCA STC SA03-43 BOMBARDIER CL-600-2B19 Installation of Safe Flight Autopower (Autothrottle) System -- 14.09.2006 10016132 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02326 TCCA STC SA95-67 BOMBARDIER DHC-8-100 Installation of Aero Consulting Services Ltd. 01.03.2007 SERIES "Improved Exhaust Outlet Shroud Assembly" BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES according to Transport Canada STC SA 95-67 10016192 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02429 TCCA SA01-65, ISSUE 4 BOMBARDIER DHC-8-100 Addition of filtration to Cabin Recirculation 1. Applicable to DHC-8-100 series with 1990 06.07.2007 SERIES Air.Addition of recirculation air filter reduces (Post-Mod 8/1127*) cabin interior, all DHC-8- BOMBARDIER DHC-8-200 potential blockage of the condenser mixer and 200 series and DHC-8-300 series with 1990 SERIES promotes peak performance of the ECS (Post-Mod 8/1128*) cabin interior.*Including BOMBARDIER DHC-8-300 system. TCCA STC SA01-65, Issue 4, dated Hunting and CD interior.2. Prior to installation SERIES 24 June 2005. of this modification the 10016270 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02554 TCCA STC C-LSA07-190/D ISSUE 2 Upgrade to Honeywell Mark V EGPWS. 02.11.2007 10016376 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02699 REV. 1 TCCA LSTC C-LSA07-342/D BOMBARDIER BD-700-1A11 Installation, Side Facing Divan, S/N 9229 Configuration. Restricted to ASN 9229. 05.03.2008 10016429 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02768 TCCA STC C-LSA08-017/D ISSUE 2 BOMBARDIER BD-700-1A10 Cabin Electronics Upgrade. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 09.07.2008 10016470 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02816 TCCA STC C-LSA08-143/D GULFSTREAM IV Installation of Interior Modifications. Aircraft Serial Number 1109 Only.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the 02.06.2008 10016471 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.02817 TCCA STC C-LSA08-151/D GULFSTREAM IV Installation of Rockwell Collins Radio Tuning Application to Aircraft Serial Number 1109 11.06.2008 Units RTU-4210 and Rockwell Collins TDR- only,The operator is responsible for th 94D (ELS/EHS) Transponder. einclusion of a 24 month check in their maintenance schedule of the Mode S transponder system toensure correct operation of the 24BIT address and the required DAPs IAW ACS M 10016605 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.03022 TCCA STC SA00-109, ISSUE 4 BOMBARDIER DHC-8-102 Installation of Enviromental Control System, Prior to installation of this modification the 19.12.2008 BOMBARDIER DHC-8-103 Low Temperature Limit System (Cold installer must determine that the BOMBARDIER DHC-8-200 Clamp)Ref. TCCA STC SA00-109, Issue 4, interrelationship between this modification and SERIES dated 19. October 2000 any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 10016606 AERO CONSULTING SERVICES LTD. EASA.IM.A.S.03023 TCCA STC SA02-4, ISSUE 1 Installation of NAI part C93602 Solid State Prior to installation of this modification the 14.10.2008 Logo Light installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 04/01/2013 Page 9/462 11.08.2006 27.10.2006
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04/01/2013 Page 1/462 - EASA

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